TEST OF TRAIL CONE SYSTEM TO CALIBRATE STATIC PORTS FOR BAROMETRIC ALTIMETERS

Abstract

An experimental trail cone stabilized static source system was fabricated and tested using various towing aircraft at speeds up to 1.12 Mach Number to determine its suitability as a 'standard' method for determining altimeter static pressure error. Flight tests were conducted at sea level, 5, 000, 10,000, 15,000, 25,000, 30,000 and 40,000 feet, to determine the static pressure defect of the trailing cone system. Test results indicated that the experimental system had a nominal 'position error' equal to = 12 feet at sea level and = 30 feet at 30,000 feet.

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Document Details

Document Type
Technical Report
Publication Date
Dec 01, 1964
Accession Number
AD0611444

Entities

People

  • Jack J. Shrager

Tags

Communities of Interest

  • Air Platforms
  • Weapons Technologies

DTIC Thesaurus Topics

  • Accuracy
  • Aircraft Industry
  • Aircrafts
  • Altimeters
  • Altitude
  • Barometric Pressure
  • Dynamic Pressure
  • Elevation
  • Low Altitude
  • Mach Number
  • Measurement
  • Military Aircraft
  • Pressure Altimeters
  • Radar
  • Sea Level
  • Static Pressure
  • Supersonic Aircraft

Readers

  • Aerospace Test and Evaluation
  • Fluid Dynamics.
  • Marine Hydrodynamics